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A C~0 plate bending element with refined shear deformation theory for composite structures

机译:具有精细剪切变形理论的C〜0板弯曲单元

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摘要

A simple C~0 finite element formulation with embedded higher-order shear deformation theory and a 3-dimensional state of stress and strain for thick and thin laminated composite plates has been presented. The assumed displacement model accounts for parabolic variation of transverse shear strains and linear variation of normal strain through the plate thickness and therefore does not require any shear correction factors. The accuracy and validity of the present element has been established through numerical evaluation of deformation and stresses against convergence study and also plate bending response under various loading, boundary conditions and lamination types. The comparison of results from the present analysis with that of other available analytical/3D elasticity solutions and published finite element results correspond fairly well.
机译:提出了一种简单的C〜0有限元公式,该公式具有嵌入的高阶剪切变形理论和厚,薄层合板的3维应力和应变状态。假定的位移模型考虑了横向剪切应变的抛物线变化和板厚度范围内法向应变的线性变化,因此不需要任何剪切​​校正因子。通过对变形和应力进行数值评估以防止收敛研究,以及在各种载荷,边界条件和层压类型下的板弯曲响应,已经确定了本单元的准确性和有效性。本分析结果与其他可用分析/ 3D弹性解决方案的结果和已发布的有限元结果的比较相当吻合。

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